通用类飞机偏航机动载荷计算方法研究
详细信息 查看官网全文
- 英文论文题名：Study on Calculation Method of General Aircraft Yaw Maneuver Load
- 论文作者：杨建国
- 英文论文作者：Yang Jianguo ; AVIC Harbin Aircraft Industry Group CO.LTD.
- 年：2016
- 作者机构：哈尔滨飞机工业集团有限责任公司;
- 论文关键词：通用飞机 ; 偏航机动 ; 方向舵 ; 飞行载荷
- 英文论文关键词：general aircraft ; yaw maneuver ; rudder ; flight load
- 会议召开时间：2016-10-31
- 会议录名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛文集（上册）
- 英文会议录名称：Discovery,Innovation and Communication——Proceedings of 7th CSAA Science and Technology Youth Forum
- 语种：中文
- 分类号：V214;V215
- 学会代码：ZGHU
- 会议名称：探索 创新 交流（第7集）——第七届中国航空学会青年科技论坛
- 会议地点：中国广东中山
- 主办单位：中国航空学会
- 学会名称：中国航空学会
- 页数：5
- 文件大小：252k
- 原文格式：O
- 会议级别：全国
摘要
本文对CCAR23部(R3版)、FAR23部(至62修正案)、CS23部(2010年版)和AP23部适航标准中关于偏航机动载荷条款进行研究,给出适航标准要求的偏航机动载荷计算方法,并用FORTRAN编写程序,以某型机为例给出相应计算结果。其中基于中国民航CCAR23部计算的结果得到中国民用航空局方认可,表明本方法符合CCAR23部要求。
We study the yaw maneuver load clause in the CCAR23,FAR23,CS23,AP23,and propose the calculation method of the yaw maneuver load which can meet the airworthiness requirement,and also design the programs with FORTRAN.We take certain airplanes as examples to obtain the corresponding calculation results.Among them the calculation results for Chinas Civil Aviation CCAR23 Department has been approved by China civil aviation authority,showing that this method is satisfying the requirements of CCAR23.
We study the yaw maneuver load clause in the CCAR23,FAR23,CS23,AP23,and propose the calculation method of the yaw maneuver load which can meet the airworthiness requirement,and also design the programs with FORTRAN.We take certain airplanes as examples to obtain the corresponding calculation results.Among them the calculation results for Chinas Civil Aviation CCAR23 Department has been approved by China civil aviation authority,showing that this method is satisfying the requirements of CCAR23.
引文
[1]中国民用航空总局.正常类、实用类、特技类和通勤类飞机适航标准(CCAR-23-R3).2005.
[2]Normal,Utility,Acrobatic,and Commuter Category Airplanes,Special Federal Aviation Regulation No.23.
[3]Certification Specifications for Normal,Utility,Aerobatic,and Commuter Category Aeroplanes CS-23.
[4]孙侠生.民用飞机结构强度刚度设计与验证指南.北京:航空工业出版社,2012.
[5]军用飞机结构强度规范(第2部分):飞行载荷(GJB67.2A-2008).
[2]Normal,Utility,Acrobatic,and Commuter Category Airplanes,Special Federal Aviation Regulation No.23.
[3]Certification Specifications for Normal,Utility,Aerobatic,and Commuter Category Aeroplanes CS-23.
[4]孙侠生.民用飞机结构强度刚度设计与验证指南.北京:航空工业出版社,2012.
[5]军用飞机结构强度规范(第2部分):飞行载荷(GJB67.2A-2008).